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Dassault Falcon 200. Dassault HU-25 Guardian. Number built. 200+. The Garrett ATF3 (US military designation F104) is a 3-spool turbofan engine developed at the California division of Garrett AiResearch. Due to mergers it is currently supported by Honeywell Aerospace. The engine's design is unusual; the core flow path is reversed twice.
Orenda Engines was a Canadian aircraft engine manufacturer and parts supplier. As part of the earlier Avro Canada conglomerate, which became Hawker Siddeley Canada , they produced a number of military jet engines from the 1950s through the 1970s, and were Canada's primary engine supplier and repair company.
Data from:Engine Data Sheets:Czechoslovakian Aero Engines [12] Walter developed families of engines based on common bore and stroke: Atom / Mikron Bore x Stroke 85 mm × 96 mm (3.35 in × 3.78 in) Minor Bore x Stroke 105 mm × 115 mm (4.14 in × 4.53 in) Junior Bore x Stroke 115 mm × 140 mm (4.53 in × 5.51 in) Major / Sagitta
Spirit of St. Louis. Fokker Trimotor. Ford Trimotor. The Wright R-790 Whirlwind was a series of nine-cylinder air-cooled radial aircraft engines built by Wright Aeronautical Corporation, with a total displacement of about 790 cubic inches (12.9 L) and around 200 horsepower (150 kW). These engines were the earliest members of the Wright ...
A Cessna Bobcat displayed with a Jacobs L-4 (R-755) engine, Pima Air & Space Museum, 2013. An early product was the 1931 L-3, a 190.4 cu in (3,120 cc) 51 hp (38 kW) three-cylinder air-cooled radial engine. Only 44 were built. By 1933, Jacobs had developed its most famous engine, the L-4 seven-cylinder air-cooled radial, with a power rating of ...
The YJ93 started life as the General Electric J79-X275, an enlarged version of the General Electric J79 turbojet with "275" meaning Mach 2.75, the engine's target operating speed. [2] This design evolved into the X279 when Mach 3 cruise became a requirement, and ultimately became the YJ93. [3] The engine used a special high-temperature JP-6 fuel.
The engine was mainly produced for Fairchild's family of training aircraft in the mid-1930s. Ranger L-440-1 Model 6.444C-2engine plate. According to H.L. Puckett, "Ranger developed a system of air cooling all cylinders to a high degree of uniformity. The system employed air under pressure, admitted through an opening in the front of the engine ...
General characteristics. Type: Twin-shaft, high-bypass turbofan engine. Length: 100 in (250 cm) Diameter: 52.2 in (133 cm) Dry weight: 1,478 lb (670 kg) Components. Compressor: Single-stage fan, 14 stage HP axial compressor. Combustors: Axial, annular.